Department of Aircraft Design - ITA

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Aircraft Design Department System Integration Aerodynamic and Impingement Analysis Freestream Mach number = 0.76 Ice droplet colliding with probe Local Mach number ≈ 2
Aircraft Design Department Winglet Design Aerodynamics analysis
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Page 3 and 4: Aircraft Design Department Staff an
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Page 15 and 16: Aircraft Design Department Aerodyna
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Aircraft Design Department Airplane
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Aircraft Design Department Comparat
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Aircraft Design Department ANN appl
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Framework for Conceptual Design of
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Aircraft Design Department Solar-po
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Aircraft Design Department New Gall
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Department of Aircraft Design - ITA

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